Linear Elastic Analysis

Perform a linear elastic analysis for comparison purposes.

Abaqus includes a three-dimensional continuum element (e.g., C3D8R) that can utilize a multilayer composite lay-up. The use of continuum elements that explicitly account for all six stress components (σ11, σ22, σ33, σ12, σ13, σ23) ensures that the material failure criteria can utilize the transverse stress components (σ33, σ13, σ23) that are neglected (or only approximated) in conventional or continuum shell elements. To demonstrate the importance of explicitly accounting for the transverse stress components, a simple linear elastic analysis is performed to allow comparison of the magnitudes of the in-plane and transverse stress components in the most highly stressed region of the model.

Model

ASCA_EP1_linear_elastic_solid.inp

Results

The image below displays the stress state for a point in the outside surface ply near the upper left-hand corner of the access door of the composite conic. The fiber constituent failure criterion is dependent on three stress components (σ11, σ12, σ13). Further examination reveals that the transverse shear stress (σ13) is negligible in comparison to the in-plane stresses (e.g., σ13 is only 0.1% of σ11). This indicates that transverse stresses will not provide a significant contribution to fiber failure. On the other hand, matrix constituent failure is driven by all six stress components. By comparing the magnitude of the out-of-plane stresses (σ33, σ13, σ23) with the magnitude of the in-plane stresses (σ22, σ12), we can see that the out-of-plane stresses will make a significant contribution to the matrix failure criterion. To accurately predict failure in the structure, matrix failure must be captured properly, because after a matrix failure event, the matrix constituent stiffness is reduced and stress redistribution causes an increase in stress in the fibers.

Because the transverse stresses are not negligible in certain regions of large composite structures, it is recommended that solid elements be used wherever possible. This will be demonstrated later when solid elements are compared with continuum shell elements (Effect of Element Type on Progressive Failure Response).